# N801GP: 1969 Douglas DC-8-71F, registration cancelled 2006-05-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 16, 2006 - Status when cancelled: Valid registration - Airframe: [Douglas DC-8-71F](https://openairdocs.org/model/douglas-dc-8-71f) (registry code 302199D) - Engine: [GE CFM56 series](https://openairdocs.org/engine/ge-cfm56-series) (registry code 30016) - Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs) - Serial number: 46039 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 5, 1994 - Certificate issued: June 19, 2003 - Last registry action: December 15, 2004 - Mode S code: AAE638 - Owner when cancelled: [Aeroturbine Inc](https://openairdocs.org/faa-owner/AEROTURBINE%20INC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N801GP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=801GP - Page: https://openairdocs.org/deregistered/N801GP-2006-05-16 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Douglas DC-8-71F: https://openairdocs.org/model/douglas-dc-8-71f.md ## Service difficulty reports (111, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RRXA011041](https://openairdocs.org/sdr/RRXA011041), Apr 30, 2001: FIRE LOOP. FAILED. ENGINE NR 1 ON TAKEOFF INTERMITTENT FIRE WARNING. AS PER QRH, ENG WAS SHUT DOWN AND FIRE LOOP TESTED. IT DID NOT RESET. DISCHARGED BOTTLE NR 1, WAITED 30 SEC, F - [SDR RRXA010029](https://openairdocs.org/sdr/RRXA010029), Mar 29, 2001: SKIN. DAMAGED. APPROX 3 INCH TEAR IN FUSELAGE SKIN AT FWD LOWER CORNER BELOW CARGO DOOR DURING FWD DOOR GUARD INSTALLATION. REPAIRED DAMAGED AREA AT LOWER FORWARD CORNER OF MC - [SDR RRXA010028](https://openairdocs.org/sdr/RRXA010028), Mar 24, 2001: OUTFLOW VALVE. FAILED. ON DESCENT, CABIN BEGAN TO CLIMB. WENT TO MAX RATE ON AUTO CONTROLLER AND MAX FLOW ON PACKS, WOULD NOT STOP CLIMB, CABIN COULD NOT BE CONTROLLED MANUALLY EITHER - [SDR RRXA10807](https://openairdocs.org/sdr/RRXA10807), Feb 21, 2001: PLATE. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO WING L/E SHIM PLATE AT I/B NR3 ENG. PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AR - [SDR RRXA10839](https://openairdocs.org/sdr/RRXA10839), Feb 15, 2001: ATTACH ANGLE. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT LWR CARGO COMPARTMENT BULKHEAD DIVIDERS ATTACH ANLGE AT STA Y+14, Z-7, X-24, DAMAGE EXCEEDED LIMITATIONS IA - [SDR RRXA10806](https://openairdocs.org/sdr/RRXA10806), Feb 15, 2001: DRIVE LINK. GOUGED. DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO R/H O/B FLAP CENTER DRIVE LINK AT STA. 319, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION// - [SDR RRXA10805](https://openairdocs.org/sdr/RRXA10805), Feb 15, 2001: ATTACH ANGLE. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT. WING REAR SPAR FLAP ATTACH FITTING AT STA. XRS98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE - [SDR RRXA10802](https://openairdocs.org/sdr/RRXA10802), Feb 15, 2001: CLIP. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ATTACH CLIP AT STA. 252 CAN'T AND R/H WING #4 MAIN INSIDE TANK THRU ACCESS HOLE 505D AND BETWEEN STRINGER 68 & - [SDR RRXA10781](https://openairdocs.org/sdr/RRXA10781), Feb 15, 2001: FITTING. GOUGED. DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO LT. WING FLAP IN FITTING AT STA. 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RE - [SDR RRXA10828](https://openairdocs.org/sdr/RRXA10828), Feb 14, 2001: SPAR. DAMAGED. DURING A MAINTENANCE VISIT FOUND ROUTED OUT DAMAGE TO C-PIT DOOR SPAR AT RT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC- - [SDR RRXA10777](https://openairdocs.org/sdr/RRXA10777), Feb 14, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO L/H WING #3 SPOILER PANEL AT #3 SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTIO - [SDR RRXA10819](https://openairdocs.org/sdr/RRXA10819), Feb 13, 2001: DOOR FRAME. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L-2 DOOR FRAME AT UPPER AFT CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOV - [SDR RRXA10813](https://openairdocs.org/sdr/RRXA10813), Feb 13, 2001: SKIN. DAMAGED. DURING A MAINTENANCE VISIT FOUND DAMAGE TO RT. ELEVATOR CONTROL TAB AT O/B CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC - [SDR RRXA10809](https://openairdocs.org/sdr/RRXA10809), Feb 12, 2001: PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H KEEL BEAM STRESS PANEL AT STA. 690-779 AND L35L-L33L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CO - [SDR RRXA10794](https://openairdocs.org/sdr/RRXA10794), Feb 12, 2001: VANE. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT. WING #4 FLAP VANE AT #4 RT. WING FLAP VANE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIV - [SDR RRXA10775](https://openairdocs.org/sdr/RRXA10775), Feb 12, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING #2 SPOILER PANEL AT #2 PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION/ - [SDR RRXA10793](https://openairdocs.org/sdr/RRXA10793), Feb 10, 2001: VANE. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT. WING I/B FLAP VANE AT RT. I/B FLAP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION - [SDR RRXA10789](https://openairdocs.org/sdr/RRXA10789), Feb 10, 2001: STRINGER. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LOWER STRINGER #55 AT STA. 495 CAN'T AND 508 CAN'T, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE A - [SDR RRXA10810](https://openairdocs.org/sdr/RRXA10810), Feb 9, 2001: PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H KEEL BEAM ACCESS COVER AT STA. 742-749 AND L33R-L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CO - [SDR RRXA10799](https://openairdocs.org/sdr/RRXA10799), Feb 9, 2001: SKIN. DAMAGED. DURING A MAINTENANCE VISIT FOUND ELONGATION DAMAGE TO NR 4 STUB WING L/E AT FWD OF SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED - [SDR RRXA10798](https://openairdocs.org/sdr/RRXA10798), Feb 9, 2001: ANGLE. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO #3 PYLON WING L/E BULLNOSE AT STA. XS220, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// - [SDR RRXA10787](https://openairdocs.org/sdr/RRXA10787), Feb 9, 2001: SKIN. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. WING L/E AT STA. XW485.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAM - [SDR RRXA10784](https://openairdocs.org/sdr/RRXA10784), Feb 9, 2001: SKIN. DAMAGED. DURING A MAINTENANCE VISIT FOUND ELONGATED HOLE DAMAGE TO WING L/E AT NR 3 ENGINE PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA - [SDR RRXA10788](https://openairdocs.org/sdr/RRXA10788), Feb 8, 2001: SKIN. DENTED. DURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO L/H I/B FLAP AT STA.XW62.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE - [SDR RRXA10859](https://openairdocs.org/sdr/RRXA10859), Feb 7, 2001: FLOOR PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO FLOOR PANEL BETWEEN TRACKS 1 & 2 AT STA. 480-560, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECT - [SDR RRXA10856](https://openairdocs.org/sdr/RRXA10856), Feb 7, 2001: FLOOR PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO UPPER CARGO COMPT. FLOOR PANEL AT STA. 580-590 X=45-55, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVE - [SDR RRXA10848](https://openairdocs.org/sdr/RRXA10848), Feb 7, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING UPPER SURFACE T/E PANEL OVER MAIN LANDING GEAR AT STA XW5 TO XW 47, DAMAGE EXCEEDED LIMITATIONS - [SDR RRXA10847](https://openairdocs.org/sdr/RRXA10847), Feb 7, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING T/E PANEL LWR. SURFACE AT STA. XRS 170, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAG - [SDR RRXA10841](https://openairdocs.org/sdr/RRXA10841), Feb 7, 2001: PANEL. DAMAGED. DURING A MAINTENANCE VISIT FOUND HOLE ELONGATED DAMAGE TO NR 3 PYLON PANEL AT PANEL 392A, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA - [SDR RRXA10827](https://openairdocs.org/sdr/RRXA10827), Feb 7, 2001: SKIN. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO A-PIT DOOR SKIN AT FWD. CENTER SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA - [SDR RRXA10804](https://openairdocs.org/sdr/RRXA10804), Feb 7, 2001: SUPPORT FITTING. GOUGED. DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO RT. WING FLAP SUPPORT FITTING AT STA. 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION/// - [SDR RRXA10854](https://openairdocs.org/sdr/RRXA10854), Feb 6, 2001: SKIN. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO R/H MLG UPPER O/B DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 - [SDR RRXA10849](https://openairdocs.org/sdr/RRXA10849), Feb 6, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING UPPER SURFACE UX-SPAR PANEL OVER MAIN LANDING GEAR AT STA. XW5 TO XW33, DAMAGE EXCEEDED LIMITAT - [SDR RRXA10846](https://openairdocs.org/sdr/RRXA10846), Feb 6, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING T/E PANEL LWR. SURFACE AT STA. XW350, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, - [SDR RRXA10845](https://openairdocs.org/sdr/RRXA10845), Feb 6, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING T/E PANEL LWR. SURFACE AT STA. XW106, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, - [SDR RRXA10842](https://openairdocs.org/sdr/RRXA10842), Feb 6, 2001: BOSS. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RETRACT PIN BOSS AT MLG SHOCK STRUT ASSSEMBLY, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TR - [SDR RRXA10785](https://openairdocs.org/sdr/RRXA10785), Feb 6, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT. WING SCISSORS PANEL AT FLAP SCISSORS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTI - [SDR RRXA10851](https://openairdocs.org/sdr/RRXA10851), Feb 5, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LWR. WING PANEL AT RT AUX. SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA - [SDR RRXA10803](https://openairdocs.org/sdr/RRXA10803), Feb 5, 2001: SKIN. TORN. DURING A MAINTENANCE VISIT FOUND TORN DAMAGE TO FLAP SKIN AT SAT. 219 AND I/B FWD. SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION//// - [SDR RRXA10853](https://openairdocs.org/sdr/RRXA10853), Feb 3, 2001: PANEL. DELAMINATED. DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT LWR. T/E PANEL AT STA XRS 219 TO XRS 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, T - [SDR RRXA10855](https://openairdocs.org/sdr/RRXA10855), Feb 2, 2001: PANEL. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO CENTER FLOOR PANEL BEHIND CENTER PADISTAL EDGE BENT & CRACKED AT SCREW HOLE, DAMAGE EXCEEDED LIMITATIONS IAW DC - [SDR RRXA10852](https://openairdocs.org/sdr/RRXA10852), Feb 2, 2001: PANEL. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO UPPER T/E PANEL HINGE FOR SPOILER AT STA. 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATE - [SDR RRXA10840](https://openairdocs.org/sdr/RRXA10840), Feb 2, 2001: BRACE. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RUDDER LOAD FEEL UNIT SUPPORT SIDE BRACE AT UPPER AND LOWER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED - [SDR RRXA10838](https://openairdocs.org/sdr/RRXA10838), Feb 2, 2001: RETAINER. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO D-PIT DOOR AT LWR. AFT DOOR RETAINER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IA - [SDR RRXA10837](https://openairdocs.org/sdr/RRXA10837), Feb 2, 2001: LONGERON. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON FITTING L34L AT STA 1260 AND C-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTI - [SDR RRXA10801](https://openairdocs.org/sdr/RRXA10801), Feb 1, 2001: STRINGER. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER #75 AND FWD SIDE STRINGER SPLICE AT STA. XCW 23 X=0 AND INSIDE R/H CENTER TANK THRU MID SPAR ACCES - [SDR RRXA10800](https://openairdocs.org/sdr/RRXA10800), Feb 1, 2001: STRINGER. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LWR STRINGER#76 AT STA. XCW47&23 AND INSIDE R/H CENTER TANK THRU MID SPAR ACCESS 560E, DAMAGE EXCEEDED LIMI - [SDR RRXA10786](https://openairdocs.org/sdr/RRXA10786), Feb 1, 2001: STRINGER. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER #76 AT STA. XCW23 AND XCW46 AND INSIDE L/H CENTER WING TANK THRU MID SPAR ACCESS HOLE 560E, DAMAGE - [SDR RRXA10835](https://openairdocs.org/sdr/RRXA10835), Jan 31, 2001: FRAME. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO D-PIT DOOR FRAME DOUBLER AT AFT TOP CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED A - [SDR RRXA10817](https://openairdocs.org/sdr/RRXA10817), Jan 31, 2001: PLATE. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO D-PIT KICK PLATE AT D-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DA All 111: https://openairdocs.org/deregistered/N801GP-2006-05-16/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.